某型导弹发射装置展开过程的动力学仿真研究  

Dynamics Simulation for the Outspread Process of A Missile Launching System

作　　者：程永强[1] 王三民[1] 陈西宏[2] 

机构地区：[1]西北工业大学,西安710068 [2]空军工程大学导弹学院,三原713800

出　　处：《弹箭与制导学报》2005年第S3期139-141,共3页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：导弹发射装置的展开性能是影响其快速反应能力的重要因素。文中给出了某型导弹发射装置展开过程的动力学计算模型,并采用ADAMS软件对此展开过程进行了动力学仿真,获得了三种驱动方式下连接铰链处的载荷变化曲线和发射筒的运动曲线。通过对比分析,对驱动方式进行了优化选择,为改善导弹发射装置的动力学性能提供了参考。The outspread performance of a missile launching system is a very important factor that affects its rapid response ability.This paper gives a model that is used to analysis the dynamics parameters of one type of missile launching system's outspread process,and research on dynamics simulation for the outspread process by ADAMS was performed.Curves of loads on joints and curves of the launching barrel's movement by three driving means were got. In the end,through contrasting,a better selection was done.This would give some reference to ameliorating the dynamical performance of missile launching system.

关 键 词：动力学仿真 导弹发射装置 展开过程 

分 类 号：TJ768.2[兵器科学与技术—武器系统与运用工程]